UC5_TC_9Preconditions: Aircraft is in operating mode M and system parameter P deviates at most +/- R % from nominal value; Input conditions / steps: Observed aircraft thrust is at value V1 and pilot input changes from A1 to A2; Expected results: Observed aircraft thrust changes and settles to value V2, respecting control objectives (settling time, overshoot, steady state error).https://repo.valu3s.eu/use-cases/aircraft-engine-controller/test-cases/uc5_tc_9https://repo.valu3s.eu/@@site-logo/logo_valu3s_green_transparent.png
UC5_TC_9
Preconditions: Aircraft is in operating mode M and system parameter P deviates at most +/- R % from nominal value; Input conditions / steps: Observed aircraft thrust is at value V1 and pilot input changes from A1 to A2; Expected results: Observed aircraft thrust changes and settles to value V2, respecting control objectives (settling time, overshoot, steady state error).